NDLI: Load-following power timeline analyses for the international space station

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Load-following power timeline analyses for the international space station

Content Provider	NASA Technical Reports Server (NTRS)
Author	Delleur, Ann Green, Robert Hojnicki, Jeffrey Fincannon Sr., James
Copyright Year	1996
Description	Spacecraft are typically complex assemblies of interconnected systems and components that have highly time-varying thermal communications, and power requirements. It is essential that systems designers be able to assess the capability of the spacecraft to meet these requirements which should represent a realistic projection of demand for these resources once the vehicle is on-orbit. To accomplish the assessment from the power standpoint, a computer code called ECAPS has been developed at NASA Lewis Research Center that performs a load-driven analysis of a spacecraft power system given time-varying distributed loading and other mission data. This program is uniquely capable of synthesizing all of the changing spacecraft conditions into a single, seamless analysis for a complete mission. This paper presents example power load timelines with which numerous data are integrated to provide a realistic assessment of the load-following capabilities of the power system. Results of analyses show how well the power system can meet the time-varying power resource demand.
File Size	645773
Page Count	12
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19960048440
Archival Resource Key	ark:/13960/t7rn83b77
Language	English
Publisher Date	1996-07-01
Access Restriction	Open
Subject Keyword	Spacecraft Propulsion And Power Schedules Electric Power Supplies International Space Station Power Modules Sts Electric Generators Spacecraft Power Supplies Complex Systems Computer Programs Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Article

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